An adjustment assembly to quickly and efficiently adjust the length of a lanyard used in conjunction with aircraft umbilical connector release mechanisms. The lanyard cable includes at least two retaining mechanisms spaced apart thereon. The adjustment assembly includes a cam portion that retains one of the retaining mechanisms when in the locked position, and allows movement of the retaining mechanisms through the adjustment assembly when in the released position. The cable length can be adjusted when in the released position.
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1. An adjustable length cable assembly system comprising:
an adjustment assembly comprising:
a housing having a first opening and a second opening positioned on opposing end walls of the housing, the housing having an extension from a side wall of the housing along a length of the housing in a direction between the end walls, the housing defining an interior cavity;
a cover for covering the interior cavity, the cover including a slot to slidably couple the cover to the housing with a cover pin, a portion of the cover disposed upon the extension, wherein the cover is slidably movable along the extension between a first position and a second position with respect to the housing;
a cam device positioned within the interior cavity and coupled to the housing, wherein the cam device includes a stop mechanism, wherein the cam device is movable between a locked position and a released position; and
a cable having at least two retaining mechanisms spaced apart thereon, the cable extending through the first and second openings and the interior cavity;
wherein when the cover is in the first position, the cam device is in the locked position and the stop mechanism retains one of the retaining mechanisms in place within the housing, wherein when the cover is in the second position, the cam device is in the released position and the first and second openings and the interior cavity provide a passageway to allow the retaining mechanisms to pass therethrough.
11. An adjustment device for a cable having at least two retaining mechanisms spaced apart thereon, the adjustment device comprising:
a housing having a base panel and a plurality of walls that define an interior space,
wherein each of the walls comprises a first edge, a second opposing edge, and a substantially planar member disposed between the first and second edge,
wherein the first edge is disposed adjacent to the base panel and each wall extends out from the base panel in a substantially orthogonal direction,
wherein the plurality of walls comprises a first wall, a second wall opposing the first wall, two side walls extending from the first wall to the second wall, and an opening positioned in each of the first wall and the second wall,
wherein the openings are aligned, and
wherein the openings are sized to allow said retaining mechanisms to pass therethrough;
a cover including a slot to slidably couple the cover to the housing and the cover covering the interior space, wherein the cover is movable along the slot between a first position and a second position with respect to the housing;
a spring having a first end and a second end, wherein the first end of the spring is coupled to the housing; and
a cam portion positioned within the interior space and rotatably coupled to the housing,
wherein the cam portion includes a channel and a recess,
wherein the spring is positioned at least partially within the channel,
wherein the second end of the spring is coupled to the cam portion,
wherein the spring is movable between a normal state and an extended state,
wherein the cam portion is movable between a locked position and an unlocked position, wherein the recess is sized to receive said cable,
wherein the recess is sized to prevent said retaining mechanism from being positioned therein when the cam portion is in the locked position,
wherein when the cover is in the first position, the spring is in the normal state and the cam portion is in the locked position, and
wherein when the cover is in the second position, the spring is in the extended state and the cam portion is in the unlocked position to provide a passageway allowing the retaining mechanisms to pass through the openings and the interior space.
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This application claims priority to U.S. Provisional Application Ser. No. 61/160,516, titled “Variable Length Lanyard,” filed on Mar. 16, 2009, which is incorporated by reference in its entirety.
The present invention relates generally to variable length lanyards. More particularly, the present invention is directed to a device or assembly for adjusting the length of a lanyard used in conjunction with aircraft umbilical connector release mechanisms.
An aircraft carrying an ordinance, such as a weapon, typically utilizes an umbilical connector and a single loop contiguous lanyard for release of the ordinance. The connector interfaces between the ordinance and a lanyard cable, and the lanyard cable is looped around an aircraft mounted post, also known as a “bail bar.”
The ordinance mounts to the connector using a receptacle on the ordinance. The spatial orientation of the receptacle can vary from one ordinance to the next. Accordingly, the spatial orientation with respect to the bail bar varies from one ordinance to the next. As a result, problems may arise if there is too much slack in the lanyard. For example, impulse loading can occur on the lanyard cable, and the lanyard may break or the connector may be damaged. In addition, too much or too little slack in the lanyard may affect the release of the ordinance, or in the case of no slack, cause premature in-flight actuation of the connector.
Most conventional lanyard designs do not allow for variations in the distance between the ordinance and the bail bar. Therefore, a number of lanyards having different lengths may be needed, so the lanyards are switched out based on the ordinance being utilized. The drawback to this conventional design is the difficulty for a user to quickly change the lanyard to suit a specific ordinance.
Therefore, a need exists for a device or mechanism that allows a user to quickly adjust the length of a lanyard and is easy to use.
Adjustment devices and systems described herein allow quick and efficient adjustment of a lanyard cable length. In one aspect, an adjustment assembly or device for a cable having at least two retaining mechanisms can include a base panel and four side walls defining a housing and arranged in a rectangular shape to form an interior cavity within the housing, a cover for covering the interior cavity, a cam device positioned in the interior cavity and coupled to the housing, and an elastic member, such as a spring, coupled to the housing and the cam device. One of the side walls and another opposing side wall each include an opening having a width or diameter that is greater than the width or diameter of the retaining mechanisms. The cover is slidably coupled to the housing, and is movable between a first position and a second position with respect to the housing. The cam device can be rotatably coupled to the housing by a cam pin. The rotation of the cam device within the interior cavity can be limited by a load pin. The cam device includes a stop mechanism, such as a recess, for retaining the cable, and a channel for receiving the elastic member. The elastic member is movable between a normal state and an extended state, and the cam device is movable between a locked position and an unlocked or released position. When the cover is in the first position, the elastic member is in the normal state, the cam device is in the locked position, and the stop mechanism prevents one of the retaining mechanisms from exiting the housing. The elastic member can be coupled to the cam device by a release pin that engages the cover when the cover is in the second position, and causes rotation of the cam device to the unlocked position. When the cover is in the second position, the elastic member is in the extended state, the cam device is in the unlocked position, and the retaining mechanisms are able to pass through the openings in the side walls and the interior cavity and the cable length can be adjusted.
In another aspect, a system is defined that includes an adjustment assembly of the present invention, and a cable having at least two retaining mechanisms extending through the housing of the adjustment assembly. The retaining mechanisms can be shaped like a ball. The openings in the side walls of the housing have a diameter that is greater than the diameter of the ball retaining mechanisms. When the adjustment assembly is in the locked position, one of the retaining mechanisms is retained within the housing and the cable is prevented from passing therethrough. When the adjustment assembly is in the unlocked or released position, the retaining mechanisms can pass through the housing and the cable length can be adjusted.
These and other aspects, objects, and features of the invention will become apparent to those having ordinary skill in the art upon consideration of the following detailed description of exemplary embodiments exemplifying the best mode for carrying out the invention as presently perceived.
A device described herein adjusts the length of a lanyard used in conjunction with release of an ordinance from an aircraft connector system. The device is generally capable of handling stresses associated with adjustment of the lanyard length. Generally, the device allows a user to quickly and easily adjust the length of a lanyard without the use of any tools.
The bottom wall 105b includes an aperture 105j sized appropriately to receive a retaining mechanism, such as a swaged ball, on a lanyard cable (not shown). The bottom wall 105b also includes a first portion 105k and a second portion 105m that extend past the side walls 105a of the housing 105. The first portion 105k includes a hole 105n extending from the bottom wall 105b towards the top wall 105c. The first portion 105k also includes a hole 105p extending a direction from one side wall 105a to the other side wall 105a. The second portion 105m includes an aperture 105q for coupling the device 100 to a connector (not shown).
The device 100 includes a cover 110 configured to couple to the housing 105. The cover 110 includes two side walls 110a, an upper wall 110b, a top wall 110c, and an opening 110e. The opening 110e is configured to receive the side walls 105a and the first portion 105k of the housing 105 such that the cover 110 rests on the extensions 105f on the housing 105. Each of the side walls 110a includes two slots 110g that align with holes 105g when the cover 110 is coupled to the housing 105. In certain embodiments, the housing 105 and the cover 110 are fabricated from aerospace grade aluminum, or any other suitable lightweight material.
The device 100 also includes a cam portion 115. The cam portion 115 includes two angled side walls 115a, a bottom wall 115b, and a top wall 115c. The top wall 115c includes a channel 115d extending lengthwise and parallel to the side walls 115a. The channel 115d is configured to receive a spring 120. The bottom wall 115b includes a recess 115e configured to receive a lanyard cable (not shown), but the recess 115e has a width that is smaller than the diameter of a swaged ball (not shown) on the lanyard cable. The cam portion 115 includes a hole 115h having a diameter similar to hole 105h of the housing 105. The cam portion 115 also includes holes 115j having a different diameter. The holes 115h, 115j extend from one side wall 115a to the other side wall 115a. The cam portion 115 further includes an angled pivot slot 115k formed by the angled side walls 115a.
The device 100 further includes a spring 120. The spring 120 includes a looped first end 120a and a looped second end 120b. A release pin 125 couples the first end 120a of the spring 120 to the cam portion 115 via holes 115j. Once assembled, the release pin 125 extends past the side walls 115a of the cam portion 115 and into a groove (not shown) in the cover 110. The spring 120 is positioned within the channel 115d upon assembly of the device 100. The second end 120b of the spring 120 is positioned into hole 105n and coupled to hole 105p in the housing 105 via a dowel pin 130.
The cam portion 115 is positioned within the cavity 105e of the housing 105. The cam portion 115 is coupled to the housing 105 by a cam pin 135. The cam pin 135 extends through holes 105h of the housing 105 and hole 115h of the cam portion 115. The cam portion 115 is rotatable within the housing 115 upon the cam pin 135. A load pin 140 extends through holes 105i of the housing 105 and rests within the angled pivot slot 115k of the cam portion 115. Once assembled, the load pin 140 restricts movement of the cam portion 115 to about 60 degrees.
The cover 110 is coupled to the housing 105 by cover pins 145. The cover pins 145 extend through holes 105g of the housing 105 and slots 110g of the cover 110. Once the cover 110 is coupled to the housing 105, the cover pins 145 allow the cover 110 to move between a first position (
The cam portion 115, the spring 120, the release pin 125, the dowel pin 130, the cam pin 135, the load pin 140, and the cover pins 145 are fabricated from corrosion-resistant steel, stainless steel, or any other suitable corrosion resistant material capable of withstanding the pulling force of a lanyard.
With respect to
With respect to
Generally, to adjust the length of a lanyard that is positioned within the opening 410 of the device 100, a user can shift the cover 110 to the released position (
Any spatial references herein, such as, for example, “top,” “bottom,” “upper,” “lower,” “above”, “below,” “rear,” “between,” “vertical,” “angular,” “beneath,” etc., are for purpose of illustration only and do not limit the specific orientation or location of the described structure.
Many modifications, features, and embodiments of the invention will become evident to those of ordinary skill in the art. It should be appreciated, therefore, that many aspects of the invention were described above by way of example only and are not intended as required or essential elements of the invention unless explicitly stated otherwise. Accordingly, it should be understood that the foregoing relates only to certain embodiments of the invention and that numerous changes may be made therein without departing from the spirit and scope of the invention. It should also be understood that the invention is not restricted to the illustrated embodiments and that various modifications can be made.
Patent | Priority | Assignee | Title |
10512294, | Mar 01 2013 | RLF Industries LLC | Impact awareness device |
10704623, | Feb 14 2017 | BULLLINE LLC; BULLINE LLC | Rope arrest-and-release device for use on utility poles |
10729201, | Mar 01 2013 | RLF Industries LLC | Impact protection apparatus |
8695174, | Feb 25 2013 | Anchor apparatus for bead chain of window covering | |
ER5282, |
Patent | Priority | Assignee | Title |
3179994, | |||
3386530, | |||
3492702, | |||
3589052, | |||
3811155, | |||
3840212, | |||
3876036, | |||
3886631, | |||
3948362, | Dec 12 1974 | ROBERT FLEMING & CO LIMITED | Personal safety equipment |
4034828, | Apr 14 1975 | Rose Manufacturing Company | Shock absorbing cable connector |
4071926, | May 09 1974 | D. B. Enterprises, Inc. | Safety device for ladder climbers |
4077094, | Sep 17 1976 | Clamping device for a rope, cable, annular bar, or the like | |
4225012, | Apr 06 1979 | Thomas & Betts International, Inc | Safety clamp device and apparatus utilizing same |
4465011, | Jul 19 1982 | Schaefer Marine, Inc. | Halyard stopper |
4521000, | Jun 06 1983 | LATCHWAYS LIMITED, A BRITISH COMPANY | Bypassing double action rope grip |
4542884, | Jun 06 1983 | Removable double action rope grip | |
4560029, | Aug 29 1984 | CREDIT LYONNAIS, NEW YORK BRANCH | Security device |
4576248, | May 02 1984 | Rescue and glider device | |
4598442, | Mar 05 1983 | HABEGGER, WILLY | Clamping device for cables and rope |
4657110, | Dec 10 1984 | D B Industries, Inc.; D B INDUSTRIES, INC | Inertia rope grab |
4669582, | Sep 26 1984 | BSI A S | Gripping device for releasably gripping a rope, wire or similar elongated flexible member |
4813469, | Jul 07 1986 | Louver blind control | |
4830340, | Dec 14 1987 | FRANKLIN, WILLIE L | Rope grip apparatus |
4912817, | Jan 21 1988 | Sophus Berendsen Marine A/S | Gripping device for an elongated flexible member |
4958415, | Jun 07 1989 | Quality Chain Corp. | Connector for lateral cable of tire chains |
5083350, | Oct 20 1989 | BSI A S | Rope gripping device |
5156240, | May 31 1991 | Rope grab | |
5265696, | Jan 31 1992 | D B Industries, Inc. | Ladder climbing safety clamp |
5323873, | Mar 18 1992 | Societe Anonyme Dite: Komet | Safety device |
5638919, | Apr 21 1994 | Froment S.A. | Anti-fall device automatically lockable on a safety rope |
5855251, | Jan 22 1997 | Security device for use with a safety line | |
5924522, | May 16 1997 | Cable grab | |
6019195, | Jul 03 1998 | Dalloz Fall Protection | Fall prevention device for vertical cable |
6095502, | Apr 15 1998 | Line grip with elongated cams | |
6948594, | Nov 16 2001 | TIFFIN SCENIC STUDIOS, INC | Rope locking device with automatic safety mechanism |
7165295, | Sep 10 2004 | Wenger Corporation | Rope lock with out-of-balance indicator and automatic lockout |
7222840, | Mar 21 2006 | Rope-guiding device | |
20060054386, | |||
20060283315, | |||
AU2008201955, | |||
DE102004016623, | |||
GB2293193, |
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